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‎.vscode/settings.json‎

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"Krasser",
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"labelrotation",
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"linalg",
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"Lince",
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"linestyle",
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"linewidth",
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"linspace",

‎CHANGELOG.md‎

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### Added
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- ENH: Allow for Alternative and Custom ODE Solvers. [#748](https://github.com/RocketPy-Team/RocketPy/pull/748)
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- ENH: Expansion of Encoders Implementation for Full Flights. [#679](https://github.com/RocketPy-Team/RocketPy/pull/679)
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- DOC: EREBUS Flight Example [#757](https://github.com/RocketPy-Team/RocketPy/pull/757))
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- DOC: Lince Flight Example [#752](https://github.com/RocketPy-Team/RocketPy/pull/752)
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- DOC: Andromeda Flight Example [#754](https://github.com/RocketPy-Team/RocketPy/pull/754)
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- ENH: create a dataset of pre-registered motors. See #664 [#744](https://github.com/RocketPy-Team/RocketPy/pull/744)
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- DOC: add Defiance flight example [#742](https://github.com/RocketPy-Team/RocketPy/pull/742)
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- ENH: Allow for Alternative and Custom ODE Solvers. [#748](https://github.com/RocketPy-Team/RocketPy/pull/748)
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### Changed
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-
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- ENH: Expansion of Encoders Implementation for Full Flights. [#679](https://github.com/RocketPy-Team/RocketPy/pull/679)
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- MNT: move piecewise functions to separate file [#746](https://github.com/RocketPy-Team/RocketPy/pull/746)
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- DOC: flight comparison improvements [#755](https://github.com/RocketPy-Team/RocketPy/pull/755)
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### Fixed
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## [v1.7.1] - 2024-12-07
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- REL: update version to 1.7.1 in configuration files [#750](https://github.com/RocketPy-Team/RocketPy/pull/750)

‎.github/CITATION.cff‎ renamed to ‎CITATION.cff‎

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‎data/motors/aerotech/AeroTech_HP-L1000W.eng‎

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; per AT announcement 5/8/14
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L1000 54 635 18 1.4000000000000001 2.194 AT
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0.004 10.664
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0.011 1268.961
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0.04 1322.279
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0.195 1226.307
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0.249 1268.961
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0.296 1242.303
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0.372 1252.966
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0.416 1215.644
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0.6 1226.307
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0.788 1215.644
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1.066 1183.653
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1.261 1167.658
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1.507 1125.004
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1.746 1087.681
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1.865 1050.359
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1.995 1045.027
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2.093 911.733
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2.158 746.448
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2.263 554.504
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2.389 405.215
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2.577 191.944
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2.693 85.308
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2.761 42.654
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3.0 0.0

‎data/motors/aerotech/AeroTech_K1000T.eng‎

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; Based on AT Instruction Sheet by C. Kobel 3/17/2010
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K1000T-P 75 396 P 1.182 2.575 AT
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0.0040 895.149
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0.015 1119.762
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0.025 1093.337
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0.095 1096.640
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0.200 1109.853
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0.300 1116.459
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0.400 1123.065
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0.500 1132.975
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0.600 1139.581
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0.700 1136.278
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0.800 1136.278
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0.900 1136.278
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1.000 1139.581
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1.100 1132.975
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1.200 1129.672
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1.300 1126.369
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1.400 1119.762
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1.500 1109.853
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1.600 1096.640
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1.700 1063.609
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1.800 1017.365
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1.900 971.121
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2.000 914.968
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2.100 868.724
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2.180 865.421
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2.200 878.634
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2.218 858.815
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2.269 670.536
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2.300 578.048
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2.332 445.923
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2.356 336.920
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2.389 224.613
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2.436 105.7
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2.500 0.0

‎data/motors/aerotech/AeroTech_K400C.eng‎

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; Aerotech K400C DMS
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K400C 54 359 14 0.493 1.194 AT
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0.008 376.374
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0.025 526.181
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0.034 548.466
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0.063 500.182
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0.178 527.419
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0.394 522.467
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0.69 502.658
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1.003 487.801
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1.494 446.944
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2.002 402.374
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2.243 377.612
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2.501 363.994
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2.658 354.089
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2.772 337.994
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2.844 304.566
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2.882 268.662
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2.929 177.044
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2.963 116.379
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3.001 99.046
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3.064 94.094
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3.123 61.904
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3.208 18.571
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3.259 0.0

‎data/motors/aerotech/AeroTech_K480W.eng‎

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; From AT Instruction Sheet by C. Kobel 3/12/10
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K480W-P 54 568 P 1.232 2.059 AT
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0.030 535.684
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0.045 860.341
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0.057 915.996
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0.098 830.194
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0.159 832.513
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0.246 795.409
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0.307 811.642
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0.398 793.090
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0.492 809.323
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0.557 823.237
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0.621 811.642
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0.689 779.176
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0.735 795.409
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0.845 767.581
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0.989 718.883
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1.091 707.288
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1.250 684.098
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1.307 667.865
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1.500 653.952
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1.606 656.271
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1.742 651.633
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1.909 628.443
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2.000 605.253
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2.250 586.701
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2.500 565.830
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2.750 547.279
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2.886 544.960
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3.000 524.089
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3.064 491.623
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3.144 417.416
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3.250 394.226
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3.292 338.571
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3.451 271.320
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3.500 231.898
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3.625 178.561
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3.700 143.777
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3.871 132.182
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4.000 88.121
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4.133 41.742
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4.246 23.190
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4.500 18.552
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4.800 0.0

‎data/motors/aerotech/AeroTech_K990DM.eng‎

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; Aerotech K990DM 54/2800
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K990DM 54 598 14 1.224 2.109 AT
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0.016 35.558
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0.024 223.805
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0.028 868.03
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0.036 1068.828
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0.044 895.222
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0.048 863.847
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0.06 840.839
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0.228 966.337
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0.286 953.788
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0.369 964.246
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0.407 993.529
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0.423 976.796
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0.498 989.345
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0.694 1024.903
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0.865 1043.728
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0.962 1054.186
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1.117 1054.186
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1.282 1029.087
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1.51 983.071
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1.589 960.063
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1.688 953.788
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1.732 968.429
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1.748 1001.895
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1.778 957.971
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1.802 891.038
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1.857 671.416
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1.913 447.611
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1.97 223.805
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2.006 129.682
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2.063 46.016
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2.097 14.641
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2.137 0.0

‎data/motors/aerotech/AeroTech_L1040DM.eng‎

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; L1040 Dark Matter
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L1040DM-P 75 681 P 2.602 4.7170000000000005 AT
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0.018 1126.167
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0.042 1036.413
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0.053 1002.543
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0.116 988.995
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0.504 1049.961
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0.794 1095.685
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1.002 1146.489
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1.252 1192.213
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1.499 1237.937
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1.753 1261.646
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1.912 1268.42
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2.095 1254.872
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2.511 1134.635
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2.772 1056.734
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3.012 966.98
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3.153 933.11
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3.217 863.677
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3.291 817.953
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3.34 758.681
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3.488 438.613
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3.552 284.505
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3.598 220.153
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3.657 167.655
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3.746 118.544
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3.88 42.337
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3.996 6.774
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4.127 0.0

‎data/motors/aerotech/AeroTech_L1940X.eng‎

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; from TMT document and posted thrust curve
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L1940X 75 560.4 P 1.8234317999999998 3.855515 AT
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0.02 48.137
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0.04 2107.333
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0.055 2289.184
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0.073 2150.122
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0.156 2101.985
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0.397 2150.122
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0.691 2155.47
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0.982 2118.03
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1.41 2000.362
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1.696 1898.739
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1.935 1839.905
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2.06 1818.511
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2.103 1652.705
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2.116 1374.58
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2.133 935.998
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2.163 534.856
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2.214 240.685
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2.244 112.32
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2.296 5.349
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2.309 0.0

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